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High Precision Dynamic 5 Axis Simulation Turntable with High Performance for HWIL Testing and Flight Motion Simulation

Jiujiang RUYA Precision Technology Co., Ltd
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    Buy cheap High Precision Dynamic 5 Axis Simulation Turntable with High Performance for HWIL Testing and Flight Motion Simulation from wholesalers
     
    Buy cheap High Precision Dynamic 5 Axis Simulation Turntable with High Performance for HWIL Testing and Flight Motion Simulation from wholesalers
    • Buy cheap High Precision Dynamic 5 Axis Simulation Turntable with High Performance for HWIL Testing and Flight Motion Simulation from wholesalers

    High Precision Dynamic 5 Axis Simulation Turntable with High Performance for HWIL Testing and Flight Motion Simulation

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    Brand Name : RUYA
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    High Precision Dynamic 5 Axis Simulation Turntable with High Performance for HWIL Testing and Flight Motion Simulation

    High Precision Dynamic 5 Axis Simulation Turntable
    Product Overview

    This high-performance HWIL testing and evaluation flight motion simulator features a five-axis simulation turntable that accurately replicates various aircraft attitudes in working environments. It realistically reproduces mechanical characteristics during actual flight and is primarily used for space attitude simulation motion experiments of inertial components.

    The system offers high dynamic response capabilities, large load capacity, and comprehensive functions including position, rate, sinusoidal oscillations, and five-axis linkage simulation. It is ideal for semi-physical simulation experiments of airborne optoelectronic systems.

    Mechanical Structure

    The mechanical configuration consists of two main components:

    • Three-axis turntable - Simulates aircraft attitude motion using O-U-T structure for roll, yaw, and pitch degrees of freedom
    • Dual-axis turntable - Simulates target relative motion using O-U structure for azimuth and pitch degrees of freedom

    Each axis provides position, rate, swing, and simulation functions, creating a comprehensive simulated motion environment for aircraft, seekers, and target simulators.

    Key Specifications
    • Maximum load: Three-axis turntable: ≥ 35 kg (including mounting fixture); Dual-axis turntable: ≥ 80 kg (including mounting fixture)
    • Load dimensions: Three-axis turntable: ≥φ300mm × 600mm; Dual-axis turntable: ≥φ300mm × 400mm
    • Intersection between three axes and two axes: ≤ 1mm radius sphere
    • Perpendicularity between axes: ±10″
    • Tilt angle rotation error: ±10″
    • Mechanical turntable dimensions: Approximately 5000 × 2500 × 3600 mm
    • Weight: Approximately 15,000 kg
    Performance Indicators


    Three-axis flight shaft system

    Two-axis target line-of-sight axis system

    Roll

    Yaw

    Pitch

    Azimuth

    Pitch

    Rotary angle range

    continuous

    ±65º

    ±65º

    ±60º

    ±60º

    Three-axis and dual-axis

    relative motion range

    With the target simulator installed, the relative limit of the pitch frame of the three-axis turntable and the pitch frame of the dual-axis turntable is ≥40º, the target simulator aperture is φ300mm, and the front end is 600mm away from the center of the turntable; the azimuth movement rotary angle range of the dual-axis turntable is ±40º.

    Minimum angular rate

    0.001 º/s

    0.001 º/s

    0.001 º/s

    0.001 º/s

    0.001 º/s

    Maximum angular rate

    400 º/s

    300 º/s

    300 º/s

    50 º/s

    50 º/s

    Maximum angular acceleration

    4000º/s 2

    3000º/s 2

    2000 º/s 2

    450 º/s 2

    450 º/s 2

    Position accuracy

    ±15″

    ±15″

    ±15″

    ±15″

    ±15″

    Position repeatability

    7.2″

    7.2″

    7.2″

    7.2″

    7.2″

    Position resolution

    3.6″

    3.6″

    3.6″

    3.6″

    3.6″

    Angular rate accuracy

    ω≤10 º/s:0.1 º/s

    ω≥10 º/s:0.1 º/s

    Angular rate stability

    ω≤1 º/s: 2×10 -2

    ω > 1 º/s: 5×10 -3

    Frequency response index


    12Hz

    8Hz

    8Hz

    4Hz

    4Hz

    Double 10, amplitude calculated based on maximum angular acceleration, peak-to-peak value 1°.




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